============ KPT ================= TIME: Mon Jun 10 13:30:54 2013 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/120308AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/120711BP_IRRE_00256_25017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_PE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SK_11175_17265.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0010.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck25Aug2011.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_21Jan2011_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00157.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_4/input.bvh Successfully Read IVT File: pdt_Run_4/input.ivt Successfully Read TLF File: /export/home/eros/D14.2d_PDT-SWDepot/Input/KPT/kpt_default.tlf Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/09_131_param.ssid Successfully Read Input PEF File: pdt_Run_4/temp.pef NOTE: This File Supercedes Any Events held within the Input Configuration File. Successfully Read KPT CMT File: /cas/ancillary/ops/SCO/cmt_limits/POST_PROBE_V11.cmt Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/120308AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/120711BP_IRRE_00256_25017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_PE_11175_17265.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/110818AP_SK_11175_17265.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0010.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck25Aug2011.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_21Jan2011_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00157.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_4/input.bvh Successfully Read IVT File: pdt_Run_4/input.ivt Successfully Read TLF File: /export/home/eros/D14.2d_PDT-SWDepot/Input/KPT/kpt_default.tlf Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/09_131_param.ssid Successfully Read Input PEF File: pdt_Run_4/temp.pef NOTE: This File Supercedes Any Events held within the Input Configuration File. Successfully Read KPT CMT File: /cas/ancillary/ops/SCO/cmt_limits/POST_PROBE_V11.cmt ------------------------------ CSAS-KPT Version: V14.1 ------------------------------ SID Suspend Values Theta_1: 0.20 degrees Theta_2: 0.50 degrees Theta_3: 1.50 degrees T_1: 60.00 seconds T_2: 240.00 seconds T_3: 1800.00 seconds T_4: 2400.00 seconds NOTE: Primary Inertial Vector TITAN_LAT_VIEW_177 WILL be propagated by a Chebyshev Polynomial from the IVT. (INITIAL CONDITIONS) NOTE: Secondary Inertial Vector TITAN_FOV_LIMB_177 WILL be propagated by a Chebyshev Polynomial from the IVT. (INITIAL CONDITIONS) ************************************************************ NOTE: MANEUVER COMMANDS Cause Turning of the Spacecraft 1.125 -> 2.000 seconds following the Command Time - the times shown in this Run Log are times that the Spacecraft Actually Starts Turning. ************************************************************ ************************************************************ NOTE: CONSTRAINT MONITOR IS SELECTED FOR THIS RUN Initial CMT Dynamic Constraints: RCS Max Rates(rad/s): 1.43000000e-02 1.43000000e-02 1.43000000e-02 RCS Max Accel(rad/s/s): 1.52700000e-04 1.24200000e-04 3.24700000e-04 RWA Max Rates(rad/s): 2.46800000e-03 2.96200000e-03 4.88600000e-03 RWA Max Accel(rad/s/s): 1.35300000e-05 1.62300000e-05 2.67800000e-05 ************************************************************ ************************************************************ * * * NOTE: ALL ERRORS, REJECTED COMMANDS, WARNINGS, * * CMT VIOLATIONS, etc, MUST BE FIXED PRIOR * * TO FINAL SEQUENCE GENERATION and UPLINK * ************************************************************ Adding/Replacing Vector TITAN_LAT_VIEW_177 to the IVT at UTC Time: 2013-335T01:25:49.000 Adding/Replacing Vector TITAN_FOV_LIMB_177 to the IVT at UTC Time: 2013-335T01:26:04.000 Adding/Replacing Vector TITAN_LAT_VIEW_178 to the IVT at UTC Time: 2013-335T01:50:49.000 Adding/Replacing Vector TITAN_FOV_LIMB_178 to the IVT at UTC Time: 2013-335T01:51:04.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T01:56:13.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_178 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #2: Secondary Inertial Vector: TITAN_FOV_LIMB_178 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T01:56:14.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_178; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_178; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T01:56:21.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 80.5456 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T01:56:19.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2013-335T01:57:41.750 Turn Magnitude for 7OFFSET (milliradians): 16.7836 Adding/Replacing Vector TITAN_FOV_LIMB_179 to the IVT at UTC Time: 2013-335T02:05:01.000 Adding/Replacing Vector TITAN_LAT_VIEW_179 to the IVT at UTC Time: 2013-335T02:05:03.000 PROCESSING Starting on PROFILE Command at 2924.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:10:13.000 ) This is Command #5 from the Event List TARGET / Command #6: Primary Inertial Vector: TITAN_LAT_VIEW_179 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #6: Secondary Inertial Vector: TITAN_FOV_LIMB_179 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 2925.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:10:14.000 ) This is Command #6 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_179; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_179; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2932.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:10:21.000 ) This is Command #7 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 39.0932 Simulated Maneuver End Time (UTC): 2013-335T02:11:00.250 Turn Magnitude for 7OFFSET (milliradians): 3.9725 Adding/Replacing Vector TITAN_FOV_LIMB_180 to the IVT at UTC Time: 2013-335T02:18:16.000 Adding/Replacing Vector TITAN_LAT_VIEW_180 to the IVT at UTC Time: 2013-335T02:18:18.000 PROCESSING Starting on PROFILE Command at 3719.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:23:28.000 ) This is Command #8 from the Event List TARGET / Command #9: Primary Inertial Vector: TITAN_LAT_VIEW_180 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #9: Secondary Inertial Vector: TITAN_FOV_LIMB_180 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 3720.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:23:29.000 ) This is Command #9 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_180; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_180; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3727.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:23:36.000 ) This is Command #10 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 36.4259 Simulated Maneuver End Time (UTC): 2013-335T02:24:12.620 Turn Magnitude for 7OFFSET (milliradians): 3.1970 Adding/Replacing Vector TITAN_FOV_LIMB_181 to the IVT at UTC Time: 2013-335T02:31:31.000 Adding/Replacing Vector TITAN_LAT_VIEW_181 to the IVT at UTC Time: 2013-335T02:31:33.000 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2013-335T02:34:24.780 PROCESSING Starting on PROFILE Command at 4514.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:36:43.000 ) This is Command #11 from the Event List TARGET / Command #12: Primary Inertial Vector: TITAN_LAT_VIEW_181 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #12: Secondary Inertial Vector: TITAN_FOV_LIMB_181 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 4515.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:36:44.000 ) This is Command #12 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN_LAT_VIEW_181; SECONDARY BODY: NEG_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_181; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 4522.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:36:51.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 34.2478 Simulated Maneuver End Time (UTC): 2013-335T02:37:25.370 Turn Magnitude for 7OFFSET (milliradians): 2.8466 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2013-335T02:45:23.000 Adding/Replacing Vector SKY_RA_DEC_175 to the IVT at UTC Time: 2013-335T02:45:24.000 PROCESSING Starting on PROFILE Command at 5324.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:50:13.000 ) This is Command #14 from the Event List PROCESSING Starting on TARGET Command at 5325.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:50:14.000 ) This is Command #15 from the Event List PRIMARY BODY: CIRS_FP1; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SKY_RA_DEC_175; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 5332.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:50:21.000 ) This is Command #16 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 323.2506 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2013-335T02:51:29.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 5630.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2013-335T02:55:19.000 ) This is Command #17 from the Event List Simulated Maneuver End Time (UTC): 2013-335T02:55:44.500 Turn Magnitude for 7OFFSET (milliradians): 303.7564 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_4/kpt_eo.plt -----------------------------------